ATE486779T1 - Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte - Google Patents
Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatteInfo
- Publication number
- ATE486779T1 ATE486779T1 AT06778954T AT06778954T ATE486779T1 AT E486779 T1 ATE486779 T1 AT E486779T1 AT 06778954 T AT06778954 T AT 06778954T AT 06778954 T AT06778954 T AT 06778954T AT E486779 T1 ATE486779 T1 AT E486779T1
- Authority
- AT
- Austria
- Prior art keywords
- icing
- aircraft engine
- air intake
- engine casing
- deicing
- Prior art date
Links
- 238000010438 heat treatment Methods 0.000 abstract 1
- 239000011810 insulating material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/13—Two-dimensional trapezoidal
- F05D2250/132—Two-dimensional trapezoidal hexagonal
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Resistance Heating (AREA)
- Resistance Heating (AREA)
- Measuring Volume Flow (AREA)
- Catching Or Destruction (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0551713A FR2887520B1 (fr) | 2005-06-22 | 2005-06-22 | Systeme de degivrage a reseaux d'elements resistifs segregues |
FR0551711A FR2887518B1 (fr) | 2005-06-22 | 2005-06-22 | Nacelle de moteur d'aeronef a dispositif de degivrage perfectionne et attenuation acoustique optimisee |
FR0551712A FR2887519B1 (fr) | 2005-06-22 | 2005-06-22 | Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif |
PCT/FR2006/050608 WO2006136748A2 (fr) | 2005-06-22 | 2006-06-19 | Systeme d'anti-givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE486779T1 true ATE486779T1 (de) | 2010-11-15 |
Family
ID=37570804
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT06778954T ATE486779T1 (de) | 2005-06-22 | 2006-06-19 | Antivereisungs- und enteisungssystem für ein flugzeugmotorengehäuse mit widerstandsmatte |
Country Status (8)
Country | Link |
---|---|
US (1) | US20100199629A1 (pt) |
EP (1) | EP1893484B1 (pt) |
JP (1) | JP2008546945A (pt) |
AT (1) | ATE486779T1 (pt) |
BR (1) | BRPI0612110A2 (pt) |
CA (1) | CA2611656C (pt) |
DE (1) | DE602006018005D1 (pt) |
WO (1) | WO2006136748A2 (pt) |
Families Citing this family (58)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006031330B4 (de) * | 2005-07-14 | 2014-03-20 | Goodrich Corp. | Für Eis empfänglicher Abschnitt eines Flugzeugs, insbesondere Flugtriebwerk- Zelleneinlasslippe, umfassend ein Eisschutzsystem, Flugtriebwerk mit einer solchen Einlasslippe sowie ein Verfahren zum Schutz einer solchen Einlasslippe vor Vereisung |
FR2898868B1 (fr) * | 2006-03-24 | 2008-12-12 | Aircelle Sa | Structure pour levre d'entree d'air de nacelle a degivrage electrique |
FR2908737B1 (fr) * | 2006-11-16 | 2009-12-04 | Airbus France | Revetement acoustique pour aeronef incorporant un systeme de traitement du givre par effet joule. |
FR2911848B1 (fr) * | 2007-01-31 | 2009-12-25 | Hispano Suiza Sa | Circuit d'alimentation en energie electrique dans un aeronef pour des equipements electriques comprenant un circuit de degivrage |
US9581033B2 (en) * | 2007-02-06 | 2017-02-28 | United Technologies Corp0Ration | Surface mounted flexible heater for gas turbine engine application |
RU2455510C2 (ru) * | 2007-02-20 | 2012-07-10 | Эрбюс Операсьон(Сас) | Способ выполнения покрытия для акустической обработки, включающее ячеистую структуру сложной формы, и покрытие для акустической обработки, полученное таким образом |
US7922121B2 (en) * | 2007-10-15 | 2011-04-12 | Rosemount Aerospace Inc. | Power distribution architecture for an ice protection system |
FR2924409B1 (fr) * | 2007-12-03 | 2010-05-14 | Airbus France | Nacelle d'aeronef comprenant des moyens d'evacuations d'air chaud |
US20090260341A1 (en) * | 2008-04-16 | 2009-10-22 | United Technologies Corporation | Distributed zoning for engine inlet ice protection |
FR2930234B1 (fr) * | 2008-04-21 | 2010-07-30 | Aircelle Sa | Systeme de degivrage et/ou d'antigivrage pour bord d'attaque de voilure d'aeronef. |
FR2940360B1 (fr) * | 2008-12-22 | 2011-10-07 | Aircelle Sa | Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef,structure d'entree d'air et structure interne fixe incorporant ledit panneau |
FR2935017B1 (fr) * | 2008-08-13 | 2012-11-02 | Snecma | Paroi interne d'une nacelle de turbomachine |
FR2936777B1 (fr) * | 2008-10-08 | 2010-10-22 | Aircelle Sa | Structure d'entree d'air pour une nacelle pour turboreacteur |
FR2938503A1 (fr) * | 2008-11-17 | 2010-05-21 | Aircelle Sa | Procede de controle d'un systeme de degivrage electrique |
FR2941439B1 (fr) * | 2009-01-28 | 2011-01-14 | Aircelle Sa | Dispositif de degivrage electrique et systeme de controle associe |
EP2391542B1 (fr) | 2009-02-02 | 2014-07-30 | Airbus Operations (S.A.S.) | Nacelle d'aeronef comprenant un systeme de traitement acoustique optimise |
FR2941675B1 (fr) * | 2009-02-02 | 2012-08-17 | Airbus France | Nacelle d'aeronef comprenant un systeme de traitement acoustique optimise. |
US8549832B2 (en) * | 2009-12-30 | 2013-10-08 | MRA Systems Inc. | Turbomachine nacelle and anti-icing system and method therefor |
US20110233340A1 (en) * | 2010-03-29 | 2011-09-29 | Christy Daniel P | Aircraft ice protection system |
US8522522B2 (en) * | 2010-07-30 | 2013-09-03 | Hamilton Sundstrand Corporation | Fan embedded power generator |
FR2976556B1 (fr) * | 2011-06-17 | 2013-12-27 | Airbus Operations Sas | Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule |
FR2980458B1 (fr) * | 2011-09-28 | 2013-08-30 | Aircelle Sa | Ensemble de levre pour nacelle de turboreacteur a degivrage electrique |
FR2984280B1 (fr) * | 2011-12-15 | 2013-12-20 | Aircelle Sa | Structure d'entree d'air pour nacelle de turboreacteur |
GB2498006B (en) * | 2011-12-22 | 2014-07-09 | Rolls Royce Plc | Gas turbine engine systems |
US8919494B2 (en) | 2012-07-31 | 2014-12-30 | Rohr, Inc. | Electric heater for integration into an aircraft acoustic panel |
FR3000724B1 (fr) * | 2013-01-07 | 2015-01-02 | Aircelle Sa | Architecture degivrage electrique a haute disponibilite d'entree d'air de nacelle a etages commutes |
FR3004165B1 (fr) | 2013-04-09 | 2015-03-27 | Aircelle Sa | Element d'aeronef necessitant un traitement contre le givre |
US9604438B2 (en) | 2014-04-30 | 2017-03-28 | The Boeing Company | Methods and apparatus for noise attenuation in an engine nacelle |
US9938852B2 (en) * | 2014-04-30 | 2018-04-10 | The Boeing Company | Noise attenuating lipskin assembly and methods of assembling the same |
US9708072B2 (en) | 2014-04-30 | 2017-07-18 | The Boeing Company | Aircraft engine nacelle bulkheads and methods of assembling the same |
US9656761B2 (en) | 2014-04-30 | 2017-05-23 | The Boeing Company | Lipskin for a nacelle and methods of making the same |
WO2016094797A2 (en) * | 2014-12-11 | 2016-06-16 | Sikorsky Aircraft Corporation | Rotor ice protection system |
FR3041937B1 (fr) * | 2015-10-05 | 2017-10-20 | Airbus Operations Sas | Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure |
CN105416593A (zh) * | 2015-12-11 | 2016-03-23 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞行器除冰系统 |
US10189572B2 (en) * | 2016-05-02 | 2019-01-29 | The Boeing Company | Systems and methods for preventing ice formation on portions of an aircraft |
US10793282B2 (en) | 2016-07-28 | 2020-10-06 | The Boeing Company | Liner assembly, engine housing, and methods of assembling the same |
IT201600098196A1 (it) * | 2016-09-30 | 2018-03-30 | Torino Politecnico | Aeromobile dotato di sistema antighiaccio strutturalmente integrato. |
US10708979B2 (en) | 2016-10-07 | 2020-07-07 | De-Ice Technologies | Heating a bulk medium |
BE1024756B1 (fr) * | 2016-11-24 | 2018-06-27 | Safran Aero Boosters S.A. | Systeme electrique degivrant de turbomachine axiale |
US9994327B1 (en) * | 2016-12-13 | 2018-06-12 | United Technologies Corporation | Aircraft nacelle anti-ice systems and methods |
FR3060651B1 (fr) * | 2016-12-20 | 2020-11-06 | Airbus Operations Sas | Structure d'entree d'air pour une nacelle d'aeronef |
FR3061132B1 (fr) * | 2016-12-27 | 2023-11-03 | Airbus Operations Sas | Structure pour ensemble propulsif d'aeronef, systeme et ensemble propulsif associes |
IT201700067602A1 (it) * | 2017-06-19 | 2018-12-19 | Leonardo Spa | Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione. |
US10655539B2 (en) * | 2017-10-16 | 2020-05-19 | Rolls-Royce North America Technologies Inc. | Aircraft anti-icing system |
FR3079818A1 (fr) * | 2018-04-10 | 2019-10-11 | Airbus Operations (S.A.S.) | Nacelle de moteur d'aeronef munie d'un systeme de protection contre le givre et procede de protection associe |
US11486308B2 (en) | 2018-07-03 | 2022-11-01 | Rohr, Inc. | Engine enclosure air inlet section |
CN112955379B (zh) | 2018-08-27 | 2024-06-18 | 迪艾斯技术有限公司 | 除冰系统 |
FR3087489B1 (fr) * | 2018-10-18 | 2022-12-09 | Airbus Operations Sas | Partie anterieure de nacelle de groupe propulsif d'aeronef comportant une voie principale de propagation d'efforts entre une levre d'entree d'air et une peau arriere d'un panneau acoustique |
FR3087420B1 (fr) * | 2018-10-19 | 2021-03-12 | Airbus Operations Sas | Nacelle de moteur d’aeronef comprenant un systeme de protection contre le givre. |
FR3098495B1 (fr) * | 2019-07-08 | 2021-07-30 | Airbus Operations Sas | Système de protection contre la formation ou l’accumulation de givre pour nacelle de moteur d’aéronef. |
US11975850B2 (en) * | 2020-04-07 | 2024-05-07 | Goodrich Corporation | Integrated busbar heater for ice protection systems |
FR3120352B1 (fr) * | 2021-03-03 | 2024-03-08 | Airbus Operations Sas | Entree d’air de nacelle munie d’un système de protection contre la glace mixte |
FR3120851A1 (fr) | 2021-03-16 | 2022-09-23 | Airbus Operations (S.A.S.) | Procédé de fonctionnement d’un système de traitement du givre combinant au moins deux tapis chauffants et paroi extérieure d’aéronef comprenant un système de traitement du givre fonctionnant selon ce procédé |
CN113955124B (zh) * | 2021-11-05 | 2024-02-13 | 天津航空机电有限公司 | 一种嵌入式进气道唇口防冰加热组件及制作方法 |
US20230167774A1 (en) * | 2021-12-01 | 2023-06-01 | Rohr, Inc. | Attachment ring insulator systems, methods, and assemblies |
FR3123049A1 (fr) * | 2021-12-20 | 2022-11-25 | Airbus Operations | Système de protection électrique contre le givre d’une nacelle d’aéronef. |
FR3130755A1 (fr) * | 2021-12-20 | 2023-06-23 | Airbus Operations | Dispositif de chauffage à matelas chauffant pour un système de protection contre le givre d’un aéronef. |
US20240017845A1 (en) * | 2022-07-15 | 2024-01-18 | The Boeing Company | Nacelle inlet assembly with acoustic panel |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2686640A (en) * | 1951-04-13 | 1954-08-17 | Jr Carr B Neel | Thermal-electric means of airfoil ice prevention |
GB1115023A (en) * | 1964-09-05 | 1968-05-22 | M H Godden Ltd | Improvements in or relating to electrical resistance heating mats |
SE8502249L (sv) * | 1985-05-07 | 1986-11-08 | Swetron Ab | Vermemadrass |
US4688745A (en) * | 1986-01-24 | 1987-08-25 | Rohr Industries, Inc. | Swirl anti-ice system |
AU611237B2 (en) * | 1987-12-14 | 1991-06-06 | Thermon Manufacturing Company | Positive temperature coefficient thermistor heating pad |
GB2259287B (en) * | 1991-09-04 | 1994-08-10 | Rolls Royce Plc | Apparatus for de-icing a surface and method of using the same |
US5657951A (en) * | 1995-06-23 | 1997-08-19 | The B.F. Goodrich Company | Electrothermal de-icing system |
FR2772341B1 (fr) * | 1997-12-12 | 2000-03-24 | Aerospatiale | Diffuseur d'air chaud pour capot d'entree d'air de moteur a reaction a circuit de degivrage |
FR2779314B1 (fr) * | 1998-05-27 | 2000-08-04 | Eurocopter France | Dispositif de chauffage a elements resistifs d'un profil aerodynamique |
US6227492B1 (en) * | 1999-08-06 | 2001-05-08 | Bell Helicopter Textron Inc. | Redundant ice management system for aircraft |
JP2003516609A (ja) * | 1999-12-10 | 2003-05-13 | サーミオン システムズ インターナショナル | 熱可塑性積層生地ヒーターおよびそれを製造する方法 |
JP2002260824A (ja) * | 2001-03-02 | 2002-09-13 | Techno Giken Kk | 可撓性面制御面発熱体 |
GB0211800D0 (en) * | 2002-05-22 | 2002-07-03 | Short Brothers Plc | An ice protection system for aircraft structures |
US6725645B1 (en) * | 2002-10-03 | 2004-04-27 | General Electric Company | Turbofan engine internal anti-ice device |
US7588212B2 (en) * | 2003-07-08 | 2009-09-15 | Rohr Inc. | Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip |
-
2006
- 2006-06-19 EP EP06778954A patent/EP1893484B1/fr not_active Not-in-force
- 2006-06-19 US US11/993,693 patent/US20100199629A1/en not_active Abandoned
- 2006-06-19 CA CA2611656A patent/CA2611656C/fr not_active Expired - Fee Related
- 2006-06-19 DE DE602006018005T patent/DE602006018005D1/de active Active
- 2006-06-19 WO PCT/FR2006/050608 patent/WO2006136748A2/fr active Application Filing
- 2006-06-19 JP JP2008517556A patent/JP2008546945A/ja active Pending
- 2006-06-19 BR BRPI0612110-1A patent/BRPI0612110A2/pt not_active Application Discontinuation
- 2006-06-19 AT AT06778954T patent/ATE486779T1/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP1893484B1 (fr) | 2010-11-03 |
BRPI0612110A2 (pt) | 2010-10-19 |
DE602006018005D1 (de) | 2010-12-16 |
US20100199629A1 (en) | 2010-08-12 |
JP2008546945A (ja) | 2008-12-25 |
WO2006136748A2 (fr) | 2006-12-28 |
CA2611656A1 (fr) | 2006-12-28 |
EP1893484A2 (fr) | 2008-03-05 |
CA2611656C (fr) | 2014-01-07 |
WO2006136748A3 (fr) | 2007-05-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |